N849AE

Part: SEAL — FOD (MAIN CABIN DOOR) · airframe 30,508 hrs · 27,464 cycles

VERY LOUD SQUEALING AND WOOSHING NOISE COMING FROM MAIN CABIN DOOR AFTER TAKE OFF-C/A-FOUND OBJECT ON DOOR SEAL AND STICKER. REMOVED FROM MAIN CABIN DOOR SEAL AND PERFORMED PRESSURIZATION CHECK IAW 21-31-00. OPS CHECK GOOD NO SQUEELING SOUND NOTED.

Part: PROXIMITY SENSOR — FAILED (SPOILER) · airframe 30,498 hrs · 27,457 cycles

SPOILER FAIL MSG ON EICAS AND OPN INDICATION WHILE AT GATE AFTER STARTUP. REMOVED AND REPLACED OB RT SIDE PROXIMITY SWITCH IAW AMM 27-63-04. OPC GOOD IAW AMM 27-63-01. NO MESSAGES NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 30,460 hrs · 27,427 cycles

ICE CONDITION ANTI ICE INOP POSTED IN FLIGHT IN ICING CONDITIONS.-C/A-PERFORMED OPS CHECK OF ANTI ICE SYSTEM PER EMB 140 AMM 30-00-00. NO DEFECTS NOTED, NO CMC MSGS POSTED. A/C OKAY FOR SERVICE.

Part: WARNING MESSAGE — FALSE INDICATION (ANTI-ICE SYSTEM) · airframe 30,386 hrs · 27,360 cycles

E2 A/ICE FAIL.-C/A-DEFERRED E2 A/ICE VALVE FAIL AS PER MEL 30-11. MTX PROCEDURES COMPLIED WITH A/C OK FOR SERVICE. PERFORMED T/S IAW EMB 140 FIM 30-80-00-810-804A FOUND TO BE TRANSITORY ON A/ICE ELECTRICAL CIRCUIT. PERFORMED OPS CHECK OF ICE DETECTION SYS. IAW EMB 140 AMM 30-80-00, OPS CHECK GOOD. MEL ITEM RESTORED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,295 hrs · 26,338 cycles

EMERGENCY LIGHT ON MAIN DOOR DOES NOT ILLUMINATE. LIGHT WOULD ONLY COME ON WHEN HOUSING ASSEMBLY AT CONNECTOR END WAS PUSHED IN. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. OPS CHECKED GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 28,984 hrs · 26,052 cycles

BAGGAGE SMOKE EICAS T GATE, CARGO DOOR CLOSED. FLIGHT ATTENDANT SAW SMOKE IN CARGO BAY. PERFORMED ETN-EM-72-034. NO SMOKE IN CARGO BAY OR CABIN. OPS CHECKED GOOD

Part: LAMP — INOPERATIVE (FLASHLIGHT) · airframe 28,863 hrs · 25,939 cycles

FLASHLIGHT IN THE REAR CABIN IS INOPERATIVE. REPLACED THE LAMP IN THE FLASHLIGHT IAW CMM 25-60-11. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (FWD CARGO) · airframe 28,804 hrs · 25,879 cycles

CARGO SMOKE WARNING DURING TAXI IN. RAN PROCEDURE AND EXTINUISHED THE CARGO BOTTLE. CFR FOUND 1 BAG ON FIRE. INSPECTED CARGO BAY IAW AMM 25-51-01, NO DAMAGE FOUND, CFR ACTUALLY FOUND NO EVIDENCE OF A BURNED BAG. REMOVED & REPLACED THE CARGO FWD SMOKE DETECTOR IAW MM 26-15-01, OPS CHECKED GOOD.

Part: IGNITER — FAILED (RT ENGINE) · airframe 28,794 hrs · 25,873 cycles

DURING TAXI, TRIED TO START THE NR 2 ENGINE, HAD A HUNG START, RAN THE CHECK LIST HAD GAS FUMES , RAN CHECK LIST AND RETURNED TO GATE. REMOVED AND REPLACED THE RT ENGINE IGNITOR A IAW AMM 74-24-01. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 28,733 hrs · 25,807 cycles

NR 1 EMERGENCY LIGHT STRIP HAS A BROKEN CONNECTOR. INSTALLED A NEW CONNECTOR AND PIN IAW SWPM 20-21-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,733 hrs · 25,807 cycles

NR 2 EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,733 hrs · 25,807 cycles

R3 LIGHT STRIP IS DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,733 hrs · 25,807 cycles

L5 EMERGENCY LIGHT STRIP DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12

Part: BRACE — CRACKED (NLG UPLOCK) · airframe 28,733 hrs · 25,807 cycles

NLG UPLOCK BOX AFT BRACE IS CRACKED. REMOVED AND REPLACED NLG UPLOCK BOX AFT BRACE IAW SRM 51-40-02.

Part: FITTING — DAMAGED (RT AILERON) · airframe 28,733 hrs · 25,807 cycles

RT AILERON DAMPER FITTING OUTBD LUG HOLE IS DAMAGED. REMOVED AND REPLACED RT AILERON DAMPER FITTING IAW SRM 51-40-02, EO EM-27MR-112.

Part: HINGE FITTING — ABNORMAL (RTAILERON) · airframe 28,733 hrs · 25,807 cycles

RT AILERON ACTUATOR HINGE FITTING LUG HOLE WORN BUSHING LOOSE IN LUG. REMOVED AND REPLACED RT AILERON ACTUATOR HINGE FITTING IAW SRM 51-40-02, EO EM-27MR-112.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,733 hrs · 25,807 cycles

SERVICE DOOR CUTOUT LOWER CENTER SILL CORRODED. REMOVED AND REPLACED SERVICE DOOR CUTOUT LOWER CENTER SILL IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,733 hrs · 25,807 cycles

FRAME 23 CRACKED BETWEEN STR 15R AND 16R. ACCOMPLISHED REPAIR OF FR 23 BETWEEN STR 15R-16R IAW SRM 53-00-04 ITEM 3 AND 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 28,733 hrs · 25,807 cycles

STRINGER 6R CRACKED AT FRAME 13. REMOVED AND REPLACED STR 6R AT FR 13 IAW SRM 51-40-02.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 28,733 hrs · 25,807 cycles

NOSE RIB ON LEFT ELEVATOR INBOARD HINGE CUTOUT INBOARD SIDE IS CRACKED. REMOVED AND REPLACED LT ELEVATOR NOSE RIB ON INBOARD HINGE CUTOUT INBOARD SIDE IAW SRM 51-40-02

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,733 hrs · 25,807 cycles

FRAME 10 CRACKED BELOW RT DV WINDOW CUTOUT. REMOVED AND REPLACED FRAME 10 BELOW RT DV WINDOW CUTOUT IAW SRM 51-40-02

Part: FITTING — DAMAGED (LT AILERON) · airframe 28,733 hrs · 25,807 cycles

LT AILERON DAMPNER FITTING IS CHAFFED ON INNER SURFACE. REMOVED AND REPLACED LT AILERON DAMPER FITTING IAW EO EM-27MR-112.

Part: FITTING — CORRODED (FUSELAGE) · airframe 28,733 hrs · 25,807 cycles

SHEAR CLIP AT FRAME 65 IS CORRODED. PERFORMED REPAIR TO SHEAR CLIP AT FRAME 65 IAW SRM 53-31-04.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,733 hrs · 25,807 cycles

FRAME 10 CRACKED BELOW LT DV WINDOW CUTOUT. REMOVED AND REPLACED FRAME 10 BELOW LT DV WINDOW CUTOUT IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,733 hrs · 25,807 cycles

CARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02.

Part: STRUCTURE — ERODED (RT WING) · airframe 28,733 hrs · 25,807 cycles

THE RT NR 2 LEADING EDGE ERODED, AND IS OUT OF LIMITS IN ONE AREA AT ZONE NR 2. REPAIRED DAMAGE IAW ERS EM-55MR-574

Part: CROSSBEAM — CRACKED (FRAME 27) · airframe 28,733 hrs · 25,807 cycles

CENTER AISLE CARBON CROSSBEAM AT FRAME 27 IS CRACKED. REMOVED AND REPLACED THE CROSSBEAM CENTER AISLE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FRAMES 16-17) · airframe 28,733 hrs · 25,807 cycles

GALLEY CENTER FLOOR SUPPORT LT ANGLE BETWEEN FRAMES 16 AND 17 CRACKED. REMOVED AND REPLACEMENT THE FLOOR SUPPORT ANGLE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FRAMES 16-17) · airframe 28,733 hrs · 25,807 cycles

GALLEY LEFT FLOOR SUPPORT LT ANGLE BETWEEN FRAMES 16 AND 17 CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE BETWEEN FRAMES 16 AND 17 IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FRAME 20) · airframe 28,733 hrs · 25,807 cycles

GALLEY CENTER AISLE FLOORBEAM AT FRAME 20 CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-21-10, AND ETN-EM-53-139R4.

Part: FLOOR SUPPORT — CORRODED (FRAMES 23-24) · airframe 28,733 hrs · 25,807 cycles

LEFT FLOOR SUPPORT HAS CORROSION BETWEEN FRAMES 23 AND 24. REPAIR THE FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 25-26) · airframe 28,733 hrs · 25,807 cycles

RIGHT FLOOR SUPPORT HAS CORROSION BETWEEN FRAMES 25 AND 26. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 28,680 hrs · 25,766 cycles

REENTER MEL 25 - 53, AFT FLASHLIGHT BRACKET BROKEN. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. MEL 25-53 RESTORED.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,388 hrs · 25,514 cycles

CAPTAIN`S FLASHLIGHT CLIP ON THE MOUNT IS BROKEN. R & R CAPTAIN`S FLASHLIGHT CRADLE. OPERATIONS CHECKED GOOD IAW AMM 33-50-16.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 28,232 hrs · 25,396 cycles

COUPLED TO FIRST OFFICER`S SIDE, DURING CLIMB OUT SPEED SELECTOR KNOB WOULD NOT CHANGE SPEED INITIALLY. AFTER 2 MIN SPEED WAS ABLE TO BE CHANGED INTERMITTENTLY. R & R NR 2 DISPLAYS CONTROL PANEL IAW AMM 34-22-04. OPERATIONS CHECKED GOOD. ACFT IS RVSM ELIGIBLE. ACFT IS COMPLIANT FOR CAT II OPERATIONS. COUPLED TO FIRST OFFICER`S SIDE, DURING CLIMB OUT ALTITUDE INDICATION CHANGED FROM 10,000 TO 10,100 WITHOUT ALTITUDE SELECTOR KNOB BEING CHANGED. ALTITUDE WOULD NOT RETURN TO 10,000 INITIALLY, BUT AFTER 2 MIN ALTITUDE WAS ABLE TO BE CHANGED TO 10,000 WITH ALTITUDE PRE SELECTOR KNOB. R & R NR 2 IC-600 IAW AMM 31-42-01. NO DEFECTS AT NR 2 IC-600 RACK CONNECTORS. OPERATIONS CHECKED GOOD IAW AMM 22-11-00, 31-42-00 & 34-22-00.

Part: CIRCUIT CARD — FAILED (NR 1) · airframe 28,193 hrs · 25,370 cycles

UPON DEPARTURE ALT SPD & HDG SELECTORS BECAME INOPERATIVE. THE SELECTORS REMAINED INOPERATIVE UNTIL SHORT FINAL. DEFERRED IAW MEL 33-02. R & R NR 1 IC 600 IAW AMM 31-42-01. OPERATIONS CHECKED GOOD IAW 31-42-00 & 22-11-00 MEL 22-2 IS RESTORED.

Part: SIGN — FADED (CABIN) · airframe 27,876 hrs · 25,104 cycles

EMERGENCY EXIT SIGN ON MAIN CABIN DOOR FADED & ILLEGIBLE. R & R IAW AMM 11-00-01.

Part: VALVE — FAILED (NR 2 PACK) · airframe 27,870 hrs · 25,096 cycles

DURING CLIMB THROUGH 12,000 FEET, NR 2 PACK VALVE FAILED MESSAGE. R & R NR 2 PACK VALVE IAW AMM 21-51-01. OPS CHECKED GOOD. LEAK CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 27,189 hrs · 24,479 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 26,871 hrs · 24,214 cycles

FIRST OFFICER'S EMERGENCY FLASHLIGHT IS BROKEN. R & R FIRST OFFICER'S EMERGENCY FLASHLIGHT IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: CRADLE — DAMAGED (CABIN) · airframe 26,871 hrs · 24,214 cycles

FORWARD PAX CABIN EMERGENCY LIGHT CRADLE STRUCTURE HAS EVIDENCE OF OVERHEATING. R & R FWD EMERGENCY LIGHT CHARGER CRADLE IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 26,871 hrs · 24,214 cycles

AFT PAX CABIN EMERGENCY LIGHT CRADLE STRUCTURE HAS EVIDENCE OF OVERHEATING. R & R AFT PAX EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: WHEEL — FAILED (NLG) · airframe 26,706 hrs · 24,059 cycles

JUST AFTER V1 NOSE SHIMMY THEN BUMP, BUMP, BUMP & THEN AIRBORNE. R & R LT NLG WHEEL ASSEMBLY IAW WC 32-700-17, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,236 hrs · 23,599 cycles

FLIGHT ATTENDANT`S FLASHLIGHT INOPERATIVE. R & R FLIGHT ATTENDANT`S FLASHLIGHT IAW AMM 33-51-01. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: BULB — BROKEN (FLASHLIGHT) · airframe 25,479 hrs · 22,948 cycles

CAPTAIN`S FLASHLIGHT BULB BROKEN. R & R FLASHLIGHT ASSY IAW AMM 33-50-00, OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 25,098 hrs · 22,560 cycles

DURING MX INSPECTION, FOUND THE CAPTAIN’S FLASHLIGHT, RED LED TO CHARGING STATUS INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R CAPTAIN’S FLASHLIGHT BATTERY IAW STANDARD PRACTICES. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 25,062 hrs · 22,522 cycles

AFT CABIN FLASHLIGHT CHARGING CRADLE INOPERATIVE. R & R AFT FLASHLIGHT CRADLE WITH SERVICEABLE ONE IAW AMM 33-50-16. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 25,023 hrs · 22,484 cycles

AFT FLASHLIGHT INTERMITTENT. R & R AFT FLASHLIGHT IAW AMM 33-50-16.

Part: WIRE — BROKEN (OVERHEAT DETECT) · airframe 25,005 hrs · 22,465 cycles

CREW RECEIVED A BLEED LEAK WARNING DURING CRUISE. CREW FOLLOWED PROCEDURES AND COULD NOT CLEAR. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND BROKEN DUCT LEAK SENSOR BY JOINT 30. REPAIRED WIRE IAW WM 20-30-00 & 20-21-00. REINSTALED THERMAL SWITCH IAW AMM 36-20-02. ACFT RETURNED TO SERVICE.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 24,835 hrs · 22,240 cycles

THE CREW REPORTED THEY RECEIVED A FLAP LOW SPEED EICAS MESSAGE DURING CRUISE FOLLOWED BY FLAP FAIL UPON FLAPS 9 SELECTION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPS CHECK FOUND WORKING PROPERLY IAW 27-53-00-700-802-A. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,572 hrs · 22,044 cycles

DURING MAINTENANCE INSPECTION FOUND THE RECHARGEABLE AFT FLASHLIGHT NEEDED TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT BATTERY IAW WC 33-700-20. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — IMPROPER PART (CABIN) · airframe 24,466 hrs · 21,964 cycles

ON FLIGHT 2805 THE FLIGHT ATTENDANT REPORTED THE FLOOR EMERGENCY LIGHT NOT CORRECT COLOR NEXT TO SEAT 2A. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN FORWARD FLOOR EMERGENCY PROXIMITY STRIP LIGHT IAW EMB 140 AMM 33-50-12THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 24,147 hrs · 21,725 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 4 LEFT SIDE EMERGENCY LIGHT STRIP HAD A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN AISLE FLOOR PROXIMITY LIGHT IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — LOOSE (CABIN) · airframe 24,147 hrs · 21,725 cycles

DURING MX INSPECTION FOUND THE HAND HELD FLASHLIGHT ON THE BACK WALL BY THE LAVATORY INOPERATIVE. ACFT REMOVED FROM SERVICE. PERFORMED OPS CHECK AND FOUND THE FLASHLIGHT TO WORK PROPERLY. THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 24,147 hrs · 21,725 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR EMERGENCY PROXIMITY LIGHT AND FLOORBOARD 261BF HAD A BROKEN CONNECTOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE FLOOR EMERGENCY PROXIMITY LIGHT AND FLOORBOARD 261BF IAW 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,041 hrs · 21,637 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW CARGO DOOR SILL IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,041 hrs · 21,637 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1, 2 & 3 BATTERY AND CHARGERS DEAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1, 2 & 3 BATTERY AND CHARGERS. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UPLOCK SWITCH — FAULTY (NLG) · airframe 24,011 hrs · 21,611 cycles

ON FLIGHT 3345 THE CREW REPORTED THAT DURING CRUISE FLIGHT AT FL 370 WITH THE GEAR UP THEY HEARD A TOTAL OF 3 LOUD CLUNKING / BANGING NOISES COMING FROM THE COCKPIT FLOORBOARD AREA. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH OPERATIONAL CHECK OF UPPER AND LWR UPLOCK SWITCHES IAW EMB AMM 32-63-05. REPLACED UPPER AND LOWER NLG UPLOCK SWITCHES IAW EMB AMM 32-61-01 UP TO AND INCLUDING STEP 3(I)(4). THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (CABIN)

FLIGHT ATTENDANT FLASHLIGHT CHARGING INTERMITTENTLY. REPLACED FORWARD FLASHLIGHT ASSY.

Part: SWITCH — FAULTY (COCKPIT) · airframe 23,111 hrs · 20,752 cycles

FLT 3151 REPORTED AFTER T/O THEY HAD A STUCK MIC ON COM 1. TRIED TO UNSTICK ALL PTT SWITCHES & RESET BREAKER FOR RMU 1. REGAINED INTERPHONE CAPABILITY BUT STILL HAD STUCK MIC. LOST INTERPHONE CAPABILITY & WAS ABLE TO TRANSMIT & RECEIVE ON COM 2 VIA F/O'S AUDIO CONTROL PANEL INTERMITTENTLY. CAPTAIN COULD NOT HEAR ATC OF F/O. RETURNED TO LAX. F/O WAS ABLE TO ESTABLISH INTERMITTENT COMMUNICATION WITH ATC ON COMM 2. F/O WAS ABLE TO COMMUNICATE WITH THE F/A AND THE PAX WHILE STILL HAVING NO COM TO INTERPHONE CAPABILITY. SHORTLY BEFORE TOUCHDOWN, THE RADIOS AND INTERPHONE SEEMED TO RETURN TO NORMAL OPERATION. REMOVED AND REPLACED THE FIRST OFFICER’S SIDE GLARESHIELD PTT SWITCH IAW EMB 140 AMM 23-51-03. PERFORMED AUDIO SYSTEM OPS TEST IAW EMB 140 AMM 23-51-00. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 22,817 hrs · 20,424 cycles

FLIGHT 3017, CREW REPORTED A STRONG SOLVENT ODOR IN THE LAVATORY. ODOR SMELLED LIKE NAIL POLISH REMOVER. AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION IN LAV FOUND NO FLUIDS RESIDUAL ODOR MAY BE FROM PREVIOUS FLIGHT. PERFORMED VISUAL INSPECTION AT CARGO BAY. CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 22,689 hrs · 20,280 cycles

FLIGHT 3007, FIRST OFFICER’S FLASHLIGHT HOLDER WAS BROKEN. REMOVED AND REPLACED FIRST OFFICER’S FLASHLIGHT CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 22,365 hrs · 19,965 cycles

ON FLIGHT 2871, THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN CABIN DOOR ROLLERS. THE OPERATIONAL CHECK WAS GOOD AMM 52-18-03. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 22,271 hrs · 19,894 cycles

FLIGHT 2968, THE CREW REPORTED THE MAIN CABIN DOOR HARD TO OPEN AND CLOSE DURING LOCK, UNLOCK SEQUENCE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND LUBRICATED IAW AMM 52-18-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 22,143 hrs · 19,796 cycles

ON FLIGHT 3015 THE CREW REPORTED THE MAIN PASSENGER DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN DOOR FRAME ROLLERS IAW EMB 140 MM 53-21-02. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — OUT OF RIG (PAX DOOR) · airframe 21,937 hrs · 19,574 cycles

FLIGHT 3066, CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. AIRCRAFT REMOVED FROM SERVICE. DURING INSPECTION FOUND LOWER ROLLER OUT OF RIG. ADJUSTED ROLLERS IAW AMM 52-18-00 AND PERFORMED FORCE CHECK IAW AMM 52-18-00. AVG LOAD 19.5KGF WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,924 hrs · 19,558 cycles

DURING MAINTENANCE INSPECTION, FOUND THE NR 4 FLOOR PROXIMITY LIGHT STRIP INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 21,831 hrs · 19,447 cycles

ON FLIGHT 3032 THE CREW REPORTED THE BAGGAGE SMOKE DETECTOR FAILED TEST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD SMOKE DETECTOR IAW EMB-140 AMM 26-15-01 AND LAMP. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — FAULTY (PAX DOOR) · airframe 21,577 hrs · 19,164 cycles

ON FLIGHT 3115 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN DOOR FRAME SEAL IAW AMM 53-21-01. REMOVED AND REPLACED MAIN DOOR TRIM SEAL IAW AMM 52-18-04. LEAK CHECK ACCOMPLISHED IAW AMM 21-31-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRANSDUCER — FAILED (RT ENGINE) · airframe 21,118 hrs · 18,762 cycles

ON FLIGHT 4368 THE CREW REPORTED THAT ON TAKEOFF RECEIVED E2 ANTI ICE FAIL MESSAGES FOLLOWED BY ICE CONDITION ANTI ICE INOPERABLE MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE TRANSDUCER IAW EMB 145 AMM 30-21-06. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERIVCE.

Part: DOOR SEAL — DEFECTIVE (PAX DOOR) · airframe 21,087 hrs · 18,736 cycles

ON FLIGHT 4379 THE CREW REPORTED THAT AT CLIMBING THROUGH 32,000 FEET THE PASSENGER DOOR STARTED MAKING A LOUD SQUEAL. CABIN ALT 6700' CAB P 7.6ASI. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR SEAL IAW EMB - 140 AMM 53-21-01. THE OPERATIONAL CHECK AND LEAK CHECK WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,175 hrs · 17,112 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CENTER FLOORBEAM CORRODED AT FRAME 20. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DAMAGED AREA BY PERFORMING CUTOUT AND INSTALLING A DOUBLER IAW EO EM-53MR-1767. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 19,175 hrs · 17,112 cycles

DURING THE MAINTENANCE BASE VISIT FOUND STRINGER 19 LEFT AT FRAME 52 CHAFED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CHAFE AT STRINGER 19 LEFT AT FRAME 52 IAW EO EM-53MR-1434. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,175 hrs · 17,112 cycles

DURING THE MAINTENANCE BASE VISIT FOUND FRAME 23 CRACKED UNDER RIGHT OUTBOARD FLOOR SUPPORT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53-MR-1760. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — STIFF (CABIN) · airframe 17,338 hrs · 15,509 cycles

FOR FLIGHT 2834 THE CREW REPORTED THE PASSENGER DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST OF THE MAIN CABIN DOOR. FORCE TO OPEN THE DOOR IS WITHIN LIMITS IAW EMB 140 AMM 52-18-00. NO DEFECTS NOTED AT THIS TIME. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,286 hrs · 15,468 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FLIGHT ATTENDANT CABIN FLASHLIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,061 hrs · 15,267 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHTS IN THE GALLEY AREA WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY PACK AND BATTERY CHARGER ASSEMBLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — FAILED (SPOILERS) · airframe 9,965 hrs · 9,281 cycles

SPOILER FAIL MESSAGE, SPOILERS SHOWED OPEN WHEN CLOSED. RETURNED TO DFW. REMOVED AND REPLACED LEFT AND RIGHT SPOILER PROXIMITY SENSORS.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,413 hrs · 9,103 cycles

CENTER OMEGA BEAM WAS FOUND CORRODED AT FRAME 25. PERFORMED CUTOUT TO REMOVE CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,413 hrs · 9,103 cycles

LT OMEGA BEAM CORRODED AT FRAME 27. PERFORMED A CUTOUT TO REMOVE CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW IC2007-145/01665, DATED 03-08-07. RETURNED AIRCRAFT TO SERVICE

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,413 hrs · 9,103 cycles

CARGO DOOR LOWER SILL CORRODED. REMOVED AND REPLACED CARGO LOWER SILL IAW EMB SRM 51-40-03. RETURN AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,413 hrs · 9,103 cycles

FOUND LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. PERFORMED CUT OUT, FABRICATED AND INSTALLED REPAIRS PARTS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE)

THE LAV FLOOR CENTER HAT BEAM WAS FOUND TO BE CORRODED. BLENDED OUT THE AREA AND REMOVED THE CORROSION. PERFORMED EDDY CURRENT INSPECTION WITH NO DISCREPANCIES. FABRICATED A DOUBLER FOR REPAIR. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-21-10, FIG 207 AND EMB IC2005-145/1805 DATED APRIL 7, 2005. (M)

Part: FUEL NOZZLE — BROKEN (APU)

DISCOVERED FUMES IN CABIN AND COCKPIT SMELLS LIKE RAW JET FUEL. WALK AROUND INSPECTION REVEALED APU LEAKING FUEL. FOUND BROKEN FUEL NOZZLE. RAI APU FUEL NOZZLE IAW MFG MM. LEAK CHECKED APU, NO LEAKS NOTED AT THIS TIME. (SW21200404647)